Journal of Projectiles, Rockets, Missiles and Guidance >
A Numerical Research on Interior Flow for Underwater Launched Missile
Received date: 2009-06-30
Online published: 2025-05-28
A two-dimensional model of interior flow was constructed for underwater missile concentric canister launcher (CCL). Two-phase flow problem was reduced to a simple high-speed gas jet. The numerical simulation indicates that the results such as the missile's velocity and displacement calculated with single-phase high-speed gas jet model and VOF model are not very different. The single phase high-speed gas jet model can give the flow details in the interior flow for underwater launched missile well and tru-ly. The simulation based on VOF model costs much more time than that based on single-phase high-speed gas jet model. A simple model of the interior flow for underwater launching is feasible.
Key words: underwater launching; interior flow; gas jet; numerical simulation
HOU Jinying , TAN Dacheng , BI Shihua . A Numerical Research on Interior Flow for Underwater Launched Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 119 -121 . DOI: 10.15892/j.cnki.djzdxb.2010.03.030
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